Future aerospace vehicles will require use of the Electrical Actuator systems for flight control elements. This report presents a proposed ELA Test Facility for dynamic evaluation of high power linear Electrical Actuators with primary emphasis on Thrust Vector Control actuators. Details of the mechanical design, power and control systems, and data acquisition capability of the test facility are presented. A test procedure for evaluating the performance of the ELA Test Facility is also included.


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    Titel :

    Strategic Avionics Technology Definition Studies. Subtask 3-1A3: Electrical Actuation (ELA) Systems Test Facility


    Beteiligte:
    J. P. Rogers (Autor:in) / K. L. Cureton (Autor:in) / J. R. Olsen (Autor:in)

    Erscheinungsdatum :

    1994


    Format / Umfang :

    53 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch